Research of the effect of heat transfer on the aerodynamic characteristics of a rectangular wing model at subsonic speeds

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This paper presents the results of parametric calculations and experiments of the influence of the surface heat exchange on the wing models integral aerodynamic characteristics at subsonic speeds. Based on the results of mathematical modeling, the Illustrative explanation of the observed phenomenon is given.

Heat exchange, aerodynamic characteristics, calculation, experiment, wing

Короткий адрес: https://sciup.org/142185819

IDR: 142185819

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